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CN109987237A - 包括在前缘区域中用更紧凑配件固定至翼盒的附接吊架的主要结构的飞行器组件 - Google Patents

包括在前缘区域中用更紧凑配件固定至翼盒的附接吊架的主要结构的飞行器组件 Download PDF

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Publication number
CN109987237A
CN109987237A CN201811616699.9A CN201811616699A CN109987237A CN 109987237 A CN109987237 A CN 109987237A CN 201811616699 A CN201811616699 A CN 201811616699A CN 109987237 A CN109987237 A CN 109987237A
Authority
CN
China
Prior art keywords
wing
assembly
box
connector
spar
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Pending
Application number
CN201811616699.9A
Other languages
English (en)
Chinese (zh)
Inventor
奥利维耶·波蒂斯
杰罗姆·科尔马格罗
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Airbus Operations SAS
Original Assignee
Airbus Operations SAS
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Airbus Operations SAS filed Critical Airbus Operations SAS
Publication of CN109987237A publication Critical patent/CN109987237A/zh
Pending legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
    • B64D27/40—Arrangements for mounting power plants in aircraft
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
    • B64D27/02—Aircraft characterised by the type or position of power plants
    • B64D27/16—Aircraft characterised by the type or position of power plants of jet type
    • B64D27/18—Aircraft characterised by the type or position of power plants of jet type within, or attached to, wings
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
    • B64D27/40—Arrangements for mounting power plants in aircraft
    • B64D27/402—Arrangements for mounting power plants in aircraft comprising box like supporting frames, e.g. pylons or arrangements for embracing the power plant
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
    • B64D27/40—Arrangements for mounting power plants in aircraft
    • B64D27/404—Suspension arrangements specially adapted for supporting vertical loads
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/28—Supporting or mounting arrangements, e.g. for turbine casing
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2240/00—Components
    • F05D2240/90—Mounting on supporting structures or systems

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Connection Of Plates (AREA)
CN201811616699.9A 2017-12-29 2018-12-27 包括在前缘区域中用更紧凑配件固定至翼盒的附接吊架的主要结构的飞行器组件 Pending CN109987237A (zh)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR1763355 2017-12-29
FR1763355A FR3076282B1 (fr) 2017-12-29 2017-12-29 Ensemble pour aeronef comprenant une structure primaire de mat d'accrochage fixee a un caisson de voilure par des attaches presentant un encombrement reduit dans la zone de bord d'attaque

Publications (1)

Publication Number Publication Date
CN109987237A true CN109987237A (zh) 2019-07-09

Family

ID=61599435

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201811616699.9A Pending CN109987237A (zh) 2017-12-29 2018-12-27 包括在前缘区域中用更紧凑配件固定至翼盒的附接吊架的主要结构的飞行器组件

Country Status (4)

Country Link
US (1) US11319079B2 (fr)
EP (1) EP3505439B1 (fr)
CN (1) CN109987237A (fr)
FR (1) FR3076282B1 (fr)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN113237661A (zh) * 2021-05-10 2021-08-10 中国商用飞机有限责任公司 一种翼吊发动机的动力学试验载荷测量装置和方法

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US11192623B2 (en) * 2018-09-14 2021-12-07 The Boeing Company Monolithic spar for a wing
GB2586476A (en) * 2019-08-20 2021-02-24 Airbus Operations Ltd Aircraft wing-pylon connection
US20230331391A1 (en) * 2022-04-15 2023-10-19 The Boeing Company Engine attachment system for aircraft and method for attaching an engine
US12030614B2 (en) 2022-11-04 2024-07-09 The Boeing Company Systems and methods for coupling a strut to a wing of an aircraft

Citations (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3952973A (en) * 1974-12-20 1976-04-27 The Boeing Company Engine mounting assembly
US4437627A (en) * 1982-03-12 1984-03-20 The Boeing Company Integrated power plant installation system
US20050082423A1 (en) * 2003-10-17 2005-04-21 Whitmer Brett D. Apparatuses and methods for attaching engines and other structures to aircraft wings
FR2887522A1 (fr) * 2005-06-28 2006-12-29 Airbus France Sas Ensemble pour aeronef comprenant un element de voilure ainsi qu'un mat d'accrochage
US20070228213A1 (en) * 2004-08-04 2007-10-04 Airbus France Aircraft Engine Unit
CN101233046A (zh) * 2005-07-29 2008-07-30 法国空中客车公司 用于飞机的包括机翼元件和挂架的组件
US20080197233A1 (en) * 2005-06-29 2008-08-21 Airbus France Engine Mounting Structure For an Aircraft
US20120080554A1 (en) * 2010-10-01 2012-04-05 Airbus Operations (S.A.S.) Aircraft engine attachment pylon comprising two front wing system attachments with orthogonal shearing pins
US20150013142A1 (en) * 2013-07-11 2015-01-15 Spirit Aerosystems, Inc. Method for mounting a pylon to an aircraft

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB0507721D0 (en) * 2005-04-16 2005-05-25 Rolls Royce Plc Gas turbine engine mounting arrangement
CN109415115B (zh) * 2016-06-29 2022-10-25 庞巴迪公司 用于飞机机翼结构的温度监测单元及相关安装方法
US10723471B2 (en) * 2017-06-14 2020-07-28 General Electric Company Method and system for mounting an aircraft engine

Patent Citations (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3952973A (en) * 1974-12-20 1976-04-27 The Boeing Company Engine mounting assembly
US4437627A (en) * 1982-03-12 1984-03-20 The Boeing Company Integrated power plant installation system
US20050082423A1 (en) * 2003-10-17 2005-04-21 Whitmer Brett D. Apparatuses and methods for attaching engines and other structures to aircraft wings
US20070228213A1 (en) * 2004-08-04 2007-10-04 Airbus France Aircraft Engine Unit
FR2887522A1 (fr) * 2005-06-28 2006-12-29 Airbus France Sas Ensemble pour aeronef comprenant un element de voilure ainsi qu'un mat d'accrochage
US20080197233A1 (en) * 2005-06-29 2008-08-21 Airbus France Engine Mounting Structure For an Aircraft
CN101233046A (zh) * 2005-07-29 2008-07-30 法国空中客车公司 用于飞机的包括机翼元件和挂架的组件
US20080217467A1 (en) * 2005-07-29 2008-09-11 Laurent Lafont Assembly For Aircraft Comprising a Wing System Element as Well as an Attachment Mast
US20120080554A1 (en) * 2010-10-01 2012-04-05 Airbus Operations (S.A.S.) Aircraft engine attachment pylon comprising two front wing system attachments with orthogonal shearing pins
US20150013142A1 (en) * 2013-07-11 2015-01-15 Spirit Aerosystems, Inc. Method for mounting a pylon to an aircraft

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN113237661A (zh) * 2021-05-10 2021-08-10 中国商用飞机有限责任公司 一种翼吊发动机的动力学试验载荷测量装置和方法
CN113237661B (zh) * 2021-05-10 2022-02-25 中国商用飞机有限责任公司 一种翼吊发动机的动力学试验载荷测量装置和方法

Also Published As

Publication number Publication date
FR3076282B1 (fr) 2020-02-07
FR3076282A1 (fr) 2019-07-05
US11319079B2 (en) 2022-05-03
EP3505439B1 (fr) 2020-04-15
EP3505439A1 (fr) 2019-07-03
US20190202572A1 (en) 2019-07-04

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